Flow structure in the wake of a space-launcher model with propulsive-jet simulation
Crossref DOI link: https://doi.org/10.1007/s12567-020-00306-8
Published Online: 2020-03-17
Published Print: 2020-09
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Schreyer, Anne-Marie
Funding for this research was provided by:
Deutsche Forschungsgemeinschaft (SFB-TR40)
Text and Data Mining valid from 2020-03-17
Version of Record valid from 2020-03-17
Article History
Received: 13 November 2019
Revised: 12 February 2020
Accepted: 24 February 2020
First Online: 17 March 2020